Please use this identifier to cite or link to this item:
http://hdl.handle.net/10397/109678
DC Field | Value | Language |
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dc.contributor | Department of Industrial and Systems Engineering | - |
dc.creator | Wang, W | - |
dc.creator | Yung, KL | - |
dc.date.accessioned | 2024-11-08T06:11:14Z | - |
dc.date.available | 2024-11-08T06:11:14Z | - |
dc.identifier.issn | 1742-6588 | - |
dc.identifier.uri | http://hdl.handle.net/10397/109678 | - |
dc.description | 2023 The 7th International Conference on Mechanical, Aeronautical and Automotive Engineering (ICMAA 2023) 24-26 February 2023, Online | en_US |
dc.language.iso | en | en_US |
dc.publisher | Institute of Physics Publishing Ltd. | en_US |
dc.rights | Content from this work may be used under the terms of the Creative Commons Attribution 3.0 licence (http://creativecommons.org/licenses/by/3.0). Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI. | en_US |
dc.rights | Published under licence by IOP Publishing Ltd | en_US |
dc.rights | The following publication Wang, W., & Yung, K. L. (2023). Analysis of a Mechanical Anchoring System for Landing on Asteroids. Journal of Physics: Conference Series, 2542(1), 012017 is available at https://doi.org/10.1088/1742-6596/2542/1/012017. | en_US |
dc.title | Analysis of a mechanical anchoring system for landing on asteroids | en_US |
dc.type | Conference Paper | en_US |
dc.identifier.volume | 2542 | - |
dc.identifier.issue | 1 | - |
dc.identifier.doi | 10.1088/1742-6596/2542/1/012017 | - |
dcterms.abstract | The landing process to an asteroid is discussed with a Nimble Lander. The miniature harpoons are chosen as the anchoring device to landing to asteroid in the Nimble Lander. The analysis results provide detailed information of the anchoring with harpoon as anchoring device. Many different designs of harpoon have been tested by simulation, the best of three designs of harpoon are analyzed for anchoring to Apophis. Instead of the modelling of the anchor as a rigid cylindrical projectile in penetration models, the deformation of the harpoon is fully considered in the anchoring analysis. The analysis provides ground base a reliable design anchoring system for landing to Asteroids. | - |
dcterms.accessRights | open access | en_US |
dcterms.bibliographicCitation | Journal of physics. Conference series, 2023, v. 2542, no. 1, 012017 | - |
dcterms.isPartOf | Journal of physics. Conference series | - |
dcterms.issued | 2023 | - |
dc.identifier.scopus | 2-s2.0-85173018270 | - |
dc.relation.conference | International Conference on Mechanical, Aeronautical and Automotive Engineering [ICMAA] | - |
dc.identifier.eissn | 1742-6596 | - |
dc.identifier.artn | 012017 | - |
dc.description.validate | 202411 bcch | - |
dc.description.oa | Version of Record | en_US |
dc.identifier.FolderNumber | OA_Scopus/WOS | en_US |
dc.description.fundingSource | Self-funded | en_US |
dc.description.pubStatus | Published | en_US |
dc.description.oaCategory | CC | en_US |
Appears in Collections: | Conference Paper |
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File | Description | Size | Format | |
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Wang_2023_J._Phys.__Conf._Ser._2542_012017.pdf | 778.45 kB | Adobe PDF | View/Open |
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